Started by upstream project "<a href='/csi/job/gplibrary_PR_Models/' class='jenkins-table__link model-link model-link--float'>gplibrary_PR_Models</a>" build number <a href='/csi/job/gplibrary_PR_Models/77' class='jenkins-table__link model-link model-link--float'>77</a>
originally caused by:
 GitHub pull request #161 of commit c8273ac60c8b8208547e2de4a4c7a9024c3ccaaa, no merge conflicts.
Building remotely on <a href='/csi/computer/windows7x64' class='jenkins-table__link model-link model-link--float'>windows7x64</a> in workspace D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek
Wiping out workspace first.
Cloning the remote Git repository
Cloning repository <a href='https://github.com/convexengineering/gplibrary'>https://github.com/convexengineering/gplibrary</a>
 &gt; git init D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek # timeout=10
Fetching upstream changes from <a href='https://github.com/convexengineering/gplibrary'>https://github.com/convexengineering/gplibrary</a>
 &gt; git --version # timeout=10
 &gt; git fetch --tags --progress <a href='https://github.com/convexengineering/gplibrary'>https://github.com/convexengineering/gplibrary</a> +refs/heads/*:refs/remotes/origin/*
 &gt; git config remote.origin.url <a href='https://github.com/convexengineering/gplibrary'>https://github.com/convexengineering/gplibrary</a> # timeout=10
 &gt; git config --add remote.origin.fetch +refs/heads/*:refs/remotes/origin/* # timeout=10
 &gt; git config remote.origin.url <a href='https://github.com/convexengineering/gplibrary'>https://github.com/convexengineering/gplibrary</a> # timeout=10
Fetching upstream changes from <a href='https://github.com/convexengineering/gplibrary'>https://github.com/convexengineering/gplibrary</a>
 &gt; git fetch --tags --progress <a href='https://github.com/convexengineering/gplibrary'>https://github.com/convexengineering/gplibrary</a> +refs/pull/*:refs/remotes/origin/pr/* +refs/heads/master:refs/remotes/origin/master
Merging Revision d2aa5c2802ceac0493de82c20e4664802e2e8d59 (refs/remotes/origin/pr/161/merge) to origin/master, UserMergeOptions{mergeRemote='origin', mergeTarget='master', mergeStrategy='default', fastForwardMode='--ff'}
 &gt; git rev-parse "origin/master^{commit}" # timeout=10
 &gt; git config core.sparsecheckout # timeout=10
 &gt; git checkout -f origin/master # timeout=3
 &gt; git merge --ff d2aa5c2802ceac0493de82c20e4664802e2e8d59 # timeout=10
 &gt; git rev-parse "HEAD^{commit}" # timeout=10
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 &gt; git show-ref --tags -d # timeout=10
Checking out Revision d2aa5c2802ceac0493de82c20e4664802e2e8d59 (origin/pr/161/merge, origin/master)
 &gt; git config core.sparsecheckout # timeout=10
 &gt; git checkout -f d2aa5c2802ceac0493de82c20e4664802e2e8d59 # timeout=3
Commit message: "Merge c8273ac60c8b8208547e2de4a4c7a9024c3ccaaa into 3824690dad9dd0d95323d63fb2ed01740e732e4c"
Using 'Changelog to branch' strategy.
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[description-setter] Description set: &lt;a title="Actuator updates" href="<a href='https://github.com/convexengineering/gplibrary/pull/161'>https://github.com/convexengineering/gplibrary/pull/161</a>"&gt;PR 161&lt;/a&gt;: Actuator updates
[Execution node] check if [windows7x64] is in [[macys, macys_VM, reynolds, reynolds-ubuntu16]]
Run condition [Execution node ] preventing perform for step [Execute shell]
[Execution node] check if [windows7x64] is in [[windows10x64, windows7x64]]
Run condition [Execution node ] enabling perform for step [Execute Windows batch command]
[mosek] $ cmd /c call C:\Users\jenkins\AppData\Local\Temp\jenkins5167294985843602440.bat

D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;echo C:\ProgramData\Oracle\Java\javapath;%CommonProgramFiles%\Microsoft Shared\Windows Live;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\Microsoft SQL Server\110\Tools\Binn\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0\;C:\Program Files\Microsoft\Web Platform Installer\;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files (x86)\Google\Chrome\Application;C:\Program Files\Common Files\Microsoft Shared\Windows Live;D:\Git\cmd 
C:\ProgramData\Oracle\Java\javapath;%CommonProgramFiles%\Microsoft Shared\Windows Live;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\Microsoft SQL Server\110\Tools\Binn\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0\;C:\Program Files\Microsoft\Web Platform Installer\;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files (x86)\Google\Chrome\Application;C:\Program Files\Common Files\Microsoft Shared\Windows Live;D:\Git\cmd

D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;REM turn on the anaconda console 

D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;call activate.bat   || exit /b 666 

(base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;REM Create a virtualenv to install everything into 

(base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;SET VENV=D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit 

(base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;virtualenv --system-site-packages D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit    || exit /b 666 
New python executable in D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\Scripts\python.exe
Installing setuptools, pip, wheel...done.

(base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;call D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\Scripts\activate.bat    || exit /b 666 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;set PATH=C:\mingw-w64\x86_64-6.4.0-posix-seh-rt_v5-rev0\mingw64\bin;D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\Scripts;D:\Anaconda2;D:\Anaconda2\Library\mingw-w64\bin;D:\Anaconda2\Library\usr\bin;D:\Anaconda2\Library\bin;D:\Anaconda2\Scripts;D:\Anaconda2\bin;C:\ProgramData\Oracle\Java\javapath;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\Microsoft SQL Server\110\Tools\Binn\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0\;C:\Program Files\Microsoft\Web Platform Installer\;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files (x86)\Google\Chrome\Application;C:\Program Files\Common Files\Microsoft Shared\Windows Live;D:\Git\cmd 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;REM set PATH=C:\mingw-w64\x86_64-7.3.0-posix-seh-rt_v5-rev0\mingw64\bin;C:\mingw-w64\x86_64-6.4.0-posix-seh-rt_v5-rev0\mingw64\bin;D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\Scripts;D:\Anaconda2;D:\Anaconda2\Library\mingw-w64\bin;D:\Anaconda2\Library\usr\bin;D:\Anaconda2\Library\bin;D:\Anaconda2\Scripts;D:\Anaconda2\bin;C:\ProgramData\Oracle\Java\javapath;C:\Program Files\Common Files\Microsoft Shared\Windows Live;C:\Windows\system32;C:\Windows;C:\Windows\System32\Wbem;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\Microsoft SQL Server\110\Tools\Binn\;C:\Program Files (x86)\Windows Kits\8.1\Windows Performance Toolkit\;C:\Program Files (x86)\Microsoft SDKs\TypeScript\1.0\;C:\Program Files\Microsoft\Web Platform Installer\;C:\Program Files\mingw-w64\x86_64-6.3.0-posix-seh-rt_v5-rev1\mingw64\bin;C:\Program Files\Mosek\7\tools\platform\win64x86\bin;D:\Anaconda2;D:\Anaconda2\Scripts;D:\Anaconda2\Library\bin;C:\Windows\System32\WindowsPowerShell\v1.0\;C:\Program Files\TortoiseSVN\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files (x86)\Google\Chrome\Application;C:\Program Files\Common Files\Microsoft Shared\Windows Live;D:\Git\cmd 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;gcc --version   || exit /b 666 
gcc (x86_64-posix-seh-rev0, Built by MinGW-W64 project) 6.4.0
Copyright (C) 2017 Free Software Foundation, Inc.
This is free software; see the source for copying conditions.  There is NO
warranty; not even for MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.


(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;REM upgdade pip 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;python -m pip install --upgrade pip 
Requirement already up-to-date: pip in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages (10.0.0)
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;REM Install coverage into the virtualenv to the coverage command blow uses the virtualenv python 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;pip install --upgrade coverage 
Collecting coverage
  Downloading <a href='https://files.pythonhosted.org/packages/a6/2c/39d7da4ea22cf32fd43a72732a4009891d17f237a0ac24bb99ed88e3a86b/coverage-4.5.1-cp27-cp27m-win_amd64.whl'>https://files.pythonhosted.org/packages/a6/2c/39d7da4ea22cf32fd43a72732a4009891d17f237a0ac24bb99ed88e3a86b/coverage-4.5.1-cp27-cp27m-win_amd64.whl</a> (178kB)
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
Installing collected packages: coverage
Successfully installed coverage-4.5.1

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;SET GPKITBUILD=D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\build_gpkit 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;if mosek == cvxopt set GPKITSOLVERS=cvxopt 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;if mosek == mosek (
msktestlic   || exit /b 666  
 python -c "__import__('mosek').Env()"   || exit /b 666  
 set GPKITSOLVERS=mosek, mosek_cli 
) 
Computer
  Platform               : Windows/64-X86  

Problem
  Name                   :                 
  Objective sense        : min             
  Type                   : LO (linear optimization problem)
  Constraints            : 1               
  Cones                  : 0               
  Scalar variables       : 5000            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Interior-point optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator - tries                  : 0                 time                   : 0.00            
Eliminator - elim's                 : 0               
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.00    
Interior-point optimizer terminated. Time: 0.00. 

Optimizer terminated. Time: 0.61    
************************************
A license was checked out correctly.
************************************

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;dir D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\build_gpkit 
 Volume in drive D is Home
 Volume Serial Number is EA39-7CA0

 Directory of D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek

File Not Found

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;python -c "import scipy; print scipy.__version__" 
1.0.1

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;python -c "import numpy; print numpy.__version__" 
1.14.2

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;python -c "import pint; print pint.__version__" 
0.8.1

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;REM Install gpkit to run the documentation examples 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;git clone --depth 1 <a href='https://github.com/convexengineering/gpkit.git'>https://github.com/convexengineering/gpkit.git</a>   || exit /b 666 
Cloning into 'gpkit'...
Checking out files:  66% (128/193)   
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(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;pip install -e D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\gpkit   || exit /b 666 
Obtaining <a href='file:///D:/jenkins/workspace/gplibrary_PR_Models/buildnode/windows7x64/optimizer/mosek/gpkit'>file:///D:/jenkins/workspace/gplibrary_PR_Models/buildnode/windows7x64/optimizer/mosek/gpkit</a>
Requirement already satisfied: numpy&gt;=1.12.1 in d:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (1.14.2)
Requirement already satisfied: pint&gt;=0.7 in d:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (0.8.1)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkit==0.7.0.0) (1.0.1)
Collecting ad (from gpkit==0.7.0.0)
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
Installing collected packages: ad, gpkit
  Running setup.py develop for gpkit
Successfully installed ad-1.3.2 gpkit

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;pip install -e D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek   || exit /b 666 
Obtaining <a href='file:///D:/jenkins/workspace/gplibrary_PR_Models/buildnode/windows7x64/optimizer/mosek'>file:///D:/jenkins/workspace/gplibrary_PR_Models/buildnode/windows7x64/optimizer/mosek</a>
Requirement already satisfied: numpy&gt;=1.12 in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.8.1)
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
Installing collected packages: gpkitmodels
  Running setup.py develop for gpkitmodels
Successfully installed gpkitmodels

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;REM Show the settings file 

(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;type D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\env\settings 
installed_solvers : mosek, mosek_cli
mosek_bin_dir : C:\Program Files\Mosek\7\tools\platform\win64x86\bin


(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;python -c "from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True, ingpkitmodels=True)" 
Obtaining <a href='file:///D:/jenkins/workspace/gplibrary_PR_Models/buildnode/windows7x64/optimizer/mosek'>file:///D:/jenkins/workspace/gplibrary_PR_Models/buildnode/windows7x64/optimizer/mosek</a>
Installing collected packages: gpkitmodels
  Found existing installation: gpkitmodels 0.0.0.0
    Uninstalling gpkitmodels-0.0.0.0:
      Successfully uninstalled gpkitmodels-0.0.0.0
  Running setup.py develop for gpkitmodels
Successfully installed gpkitmodels
Cloning into 'shopping'...
adding test for 'test.py'
Using solver 'mosek'
Solving for 25 variables.
Solving took 1.46 seconds.
Using solver 'mosek'
Solving for 25 variables.
Solving took 0.274 seconds.
Using solver 'mosek_cli'
Solving for 25 variables.
Solving took 0.855 seconds.

Running tests...
----------------------------------------------------------------------
...
----------------------------------------------------------------------
Ran 3 tests in 3.227s

OK

Generating XML reports...
Cloning into 'gassolar'...
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Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1)
Requirement already satisfied: pytz&gt;=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3)
Requirement already satisfied: numpy&gt;=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.2)
Requirement already satisfied: six&gt;=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil-&gt;pandas) (1.11.0)
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
Collecting git+<a href='https://github.com/hoburg/gpfit.git'>https://github.com/hoburg/gpfit.git</a>
  Cloning <a href='https://github.com/hoburg/gpfit.git'>https://github.com/hoburg/gpfit.git</a> to c:\users\jenkins\appdata\local\temp\pip-req-build-frkrjz
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint&gt;=0.7 in d:\anaconda2\lib\site-packages (from gpkit-&gt;gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit-&gt;gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
  Running setup.py bdist_wheel for gpfit: started
  Running setup.py bdist_wheel for gpfit: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-jmq39n\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
Installing collected packages: gpfit
Successfully installed gpfit-0.1
Processing d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gassolar
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint&gt;=0.7 in d:\anaconda2\lib\site-packages (from gpkit-&gt;gassolar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit-&gt;gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas-&gt;gassolar==0.0.0.0) (2.6.1)
Requirement already satisfied: pytz&gt;=2011k in d:\anaconda2\lib\site-packages (from pandas-&gt;gassolar==0.0.0.0) (2017.3)
Requirement already satisfied: six&gt;=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil-&gt;pandas-&gt;gassolar==0.0.0.0) (1.11.0)
Building wheels for collected packages: gassolar
  Running setup.py bdist_wheel for gassolar: started
  Running setup.py bdist_wheel for gassolar: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-wtgiz9\wheels\27\2e\a1\4da6c2a362dd12f22914b14a911a1d857b1a34a0ded2fc094b
Successfully built gassolar
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
Installing collected packages: gassolar
Successfully installed gassolar-0.0.0.0
adding test for 'gassolar/gas/gas.py'
adding test for 'gassolar/solar/solar.py'
Using solver 'mosek'
Solving for 609 variables.
Solving took 59 seconds.
Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685
Beginning signomial solve.
Solving took 4 GP solves and 6.48 seconds.
Warning: Variable [P_{shaft-max}_Mission.1/Climb.1/FlightSegment.2/AircraftPerf.2/EnginePerf.2_(0,)**-1*P_{total}_Miss could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685
Using solver 'mosek'
Solving for 609 variables.
Solving took 2.45 seconds.
Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685
Beginning signomial solve.
Solving took 4 GP solves and 23.2 seconds.
Warning: Variable [P_{shaft-max}_Mission.1/Climb.1/FlightSegment.2/AircraftPerf.2/EnginePerf.2_(0,)**-1*P_{total}_Miss could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685
Using solver 'mosek'
Solving for 1437 variables.
Solving took 8.09 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.1925 but bound is 150000.0000
Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 131552.1335 but bound is 150000.0000
Beginning signomial solve.
Solving took 4 GP solves and 90.3 seconds.
Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134553.0985 but bound is 150000.0000
Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 134553.9076 but bound is 150000.0000
Using solver 'mosek_cli'
Solving for 1437 variables.
Solving took 20.3 seconds.
Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.0147 but bound is 150000.0000
Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 131552.3302 but bound is 150000.0000
Beginning signomial solve.
Solving took 4 GP solves and 385 seconds.
Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134552.5355 but bound is 150000.0000
Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 134553.8810 but bound is 150000.0000

Running tests...
----------------------------------------------------------------------
..D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
..
----------------------------------------------------------------------
Ran 4 tests in 625.508s

OK

Generating XML reports...
Cloning into 'jho'...
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1)
Requirement already satisfied: pytz&gt;=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3)
Requirement already satisfied: numpy&gt;=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.2)
Requirement already satisfied: six&gt;=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil-&gt;pandas) (1.11.0)
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
Collecting git+<a href='https://github.com/hoburg/gpfit.git'>https://github.com/hoburg/gpfit.git</a>
  Cloning <a href='https://github.com/hoburg/gpfit.git'>https://github.com/hoburg/gpfit.git</a> to c:\users\jenkins\appdata\local\temp\pip-req-build-er6lo3
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+<a href='https://github.com/hoburg/gpfit.git'>https://github.com/hoburg/gpfit.git</a> in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint&gt;=0.7 in d:\anaconda2\lib\site-packages (from gpkit-&gt;gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit-&gt;gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
  Running setup.py bdist_wheel for gpfit: started
  Running setup.py bdist_wheel for gpfit: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-k72ccw\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
adding test for 'model/jho.py'
adding test for 'model/print_perf.py'
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.988575079220794e-14.
Allowing negative dual variable(s) as small as -8.121888578349612e-14.
Allowing negative dual variable(s) as small as -1.4806775597286936e-13.
Allowing negative dual variable(s) as small as -1.5951432882910233e-13.
Solving took 4 GP solves and 6.56 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.958000577956703e-14.
Allowing negative dual variable(s) as small as -8.099120332727416e-14.
Allowing negative dual variable(s) as small as -1.5018498597529906e-13.
Allowing negative dual variable(s) as small as -1.4915369286883084e-13.
Solving took 4 GP solves and 7.21 seconds.
Allowing negative dual variable(s) as small as -5.246410944570457e-13.
Allowing negative dual variable(s) as small as -5.117642420948698e-13.
Allowing negative dual variable(s) as small as -5.160386007396767e-13.
Allowing negative dual variable(s) as small as -5.134018210561919e-13.
Allowing negative dual variable(s) as small as -2.3112284655568693e-13.
Allowing negative dual variable(s) as small as -1.8337870284768076e-14.
Allowing negative dual variable(s) as small as -1.2600776541984993e-12.
Allowing negative dual variable(s) as small as -1.2590575283744077e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -2.1264674049392696e-14.
Allowing negative dual variable(s) as small as -1.1406674216285495e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.434131440738155e-11.
Allowing negative dual variable(s) as small as -6.449789449259642e-12.
Allowing negative dual variable(s) as small as -1.9339292765642808e-11.
Allowing negative dual variable(s) as small as -1.935445807577064e-11.
Solving took 4 GP solves and 6.33 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 4.33 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.229063709810688e-13.
Allowing negative dual variable(s) as small as -5.139690756328363e-13.
Allowing negative dual variable(s) as small as -5.15861658945127e-13.
Allowing negative dual variable(s) as small as -5.155563476133551e-13.
Allowing negative dual variable(s) as small as -2.334230898848322e-13.
Allowing negative dual variable(s) as small as -1.931896483065021e-14.
Allowing negative dual variable(s) as small as -1.2600088073605464e-12.
Allowing negative dual variable(s) as small as -1.2591489266175482e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -1.9172597537364666e-14.
Allowing negative dual variable(s) as small as -1.1364845696471004e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.434122985739979e-11.
Allowing negative dual variable(s) as small as -6.449656439437706e-12.
Allowing negative dual variable(s) as small as -1.9339133260127356e-11.
Allowing negative dual variable(s) as small as -1.9354556859479336e-11.
Solving took 4 GP solves and 16.7 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 14.1 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417

Running tests...
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....
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Ran 4 tests in 158.827s

OK

Generating XML reports...
Cloning into 'turbofan'...
Processing d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\turbofan
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.8.1)
Building wheels for collected packages: turbofan
  Running setup.py bdist_wheel for turbofan: started
  Running setup.py bdist_wheel for turbofan: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-fvjdwn\wheels\dd\4b\7e\92f7e903621e519a129c420d5ea6a42fdf8b25b6fdfc976a15
Successfully built turbofan
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
Installing collected packages: turbofan
Successfully installed turbofan-0.0.0.0
adding test for 'turbofan/engine_validation.py'
Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(0,) + F_{8}_Engine/EnginePerformance/ThrustPerform... &gt;= F_Engine/EnginePerformance/ThrustPerformance_(0,) [N]...] is not tight because the left hand side evaluated to 24184.7528315 newton but the right hand side evaluated to 24184.16 newton (Allowable error: 0.0001%, Actual error: 0.0025%)

Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(1,) + F_{8}_Engine/EnginePerformance/ThrustPerform... &gt;= F_Engine/EnginePerformance/ThrustPerformance_(1,) [N]...] is not tight because the left hand side evaluated to 26232.8485055 newton but the right hand side evaluated to 26232.36 newton (Allowable error: 0.0001%, Actual error: 0.0019%)


Running tests...
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.
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Ran 1 test in 10.144s

OK

Generating XML reports...
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Collecting git+<a href='https://github.com/hoburg/turbofan.git'>https://github.com/hoburg/turbofan.git</a>
  Cloning <a href='https://github.com/hoburg/turbofan.git'>https://github.com/hoburg/turbofan.git</a> to c:\users\jenkins\appdata\local\temp\pip-req-build-ob4dbk
Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+<a href='https://github.com/hoburg/turbofan.git'>https://github.com/hoburg/turbofan.git</a> in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (0.8.1)
Building wheels for collected packages: turbofan
  Running setup.py bdist_wheel for turbofan: started
  Running setup.py bdist_wheel for turbofan: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-vd3iwk\wheels\49\e6\3a\5de0d21c0f148404ea8d883f76e050c82d4e9a0e6f59ce69a5
Successfully built turbofan
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
adding test for 'SP_aircraft.py'
Solving over 9 passes.
Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... &gt;= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2519604.0123 force_pound * meter but the right hand side evaluated to 2468461.16505 force_pound * meter (Allowable error: 0.1%, Actual error: 2.1%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... &gt;= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4573288 force_pound but the right hand side evaluated to 32399.9999986 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... &gt;= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116789 meter but the right hand side evaluated to 1.96396105373 meter (Allowable error: 0.1%, Actual error: 11%)

Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 0) + F_{8}_Mission/Aircraft/En... &gt;= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 0) [N]...] is not tight because the left hand side evaluated to 48608.8384865 newton but the right hand side evaluated to 48529.6773293 newton (Allowable error: 0.1%, Actual error: 0.16%)

Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(1, 0) + F_{8}_Mission/Aircraft/En... &gt;= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(1, 0) [N]...] is not tight because the left hand side evaluated to 49704.433683 newton but the right hand side evaluated to 49411.1909476 newton (Allowable error: 0.1%, Actual error: 0.59%)

Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(3, 0) + F_{8}_Mission/Aircraft/En... &gt;= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(3, 0) [N]...] is not tight because the left hand side evaluated to 18949.0356968 newton but the right hand side evaluated to 18923.0387786 newton (Allowable error: 0.1%, Actual error: 0.14%)

Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(4, 0) + F_{8}_Mission/Aircraft/En... &gt;= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(4, 0) [N]...] is not tight because the left hand side evaluated to 16591.96376 newton but the right hand side evaluated to 16565.7570743 newton (Allowable error: 0.1%, Actual error: 0.16%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1002814.71469 joule / kilogram but the right hand side evaluated to 1.15242775365 megajoule / kilogram (Allowable error: 0.1%, Actual error: 7.1%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 895044.271599 joule / kilogram but the right hand side evaluated to 0.897473138651 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.13%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1072947.52332 joule / kilogram but the right hand side evaluated to 1.19571031106 megajoule / kilogram (Allowable error: 0.1%, Actual error: 5.6%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 596870.763439 joule / kilogram but the right hand side evaluated to 0.615557232636 megajoule / kilogram (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 786925.158746 joule / kilogram but the right hand side evaluated to 0.790364139459 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.22%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... &gt;= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.3465564175 meter but the right hand side evaluated to 16.3967788764 meter (Allowable error: 0.1%, Actual error: 12%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 11.085408605729263 but the right hand side evaluated to 4.680789543738308 (Allowable error: 0.1%, Actual error: 58%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 9.791744132478623 but the right hand side evaluated to 4.68078953830301 (Allowable error: 0.1%, Actual error: 52%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.2291306103657 but the right hand side evaluated to 4.680789545365954 (Allowable error: 0.1%, Actual error: 43%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4249281482 meter but the right hand side evaluated to 18.1659873949 meter (Allowable error: 0.1%, Actual error: 1.4%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4249281482 meter but the right hand side evaluated to 18.2854643566 meter (Allowable error: 0.1%, Actual error: 0.76%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.31012133478469917 but the right hand side evaluated to 0.19292703883365064 (Allowable error: 0.1%, Actual error: 2.5%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.24134487717702946 but the right hand side evaluated to 0.17650292398914244 (Allowable error: 0.1%, Actual error: 1.4%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.275040225461089 but the right hand side evaluated to 4.615986508742763 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.453668152174349 but the right hand side evaluated to 4.6463456646470505 (Allowable error: 0.1%, Actual error: 38%)


Solves with these variables bounded:
   value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission

Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... &gt;= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2504976.58428 force_pound * meter but the right hand side evaluated to 2454470.88465 force_pound * meter (Allowable error: 0.1%, Actual error: 2.1%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... &gt;= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4820825 force_pound but the right hand side evaluated to 32399.9999989 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... &gt;= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116796 meter but the right hand side evaluated to 1.96383158169 meter (Allowable error: 0.1%, Actual error: 11%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 982256.982216 joule / kilogram but the right hand side evaluated to 1.20547092622 megajoule / kilogram (Allowable error: 0.1%, Actual error: 10%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1151137.31421 joule / kilogram but the right hand side evaluated to 1.8837949594 megajoule / kilogram (Allowable error: 0.1%, Actual error: 25%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... &gt;= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4111617668 meter but the right hand side evaluated to 16.4524802692 meter (Allowable error: 0.1%, Actual error: 12%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 11.089310474512963 but the right hand side evaluated to 4.731321152808482 (Allowable error: 0.1%, Actual error: 57%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 9.749135740708299 but the right hand side evaluated to 4.731321145990996 (Allowable error: 0.1%, Actual error: 51%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.197834367904546 but the right hand side evaluated to 4.73132115511503 (Allowable error: 0.1%, Actual error: 42%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4749957573 meter but the right hand side evaluated to 18.2223415545 meter (Allowable error: 0.1%, Actual error: 1.4%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4749957573 meter but the right hand side evaluated to 18.3384465168 meter (Allowable error: 0.1%, Actual error: 0.74%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.30927823000554877 but the right hand side evaluated to 0.19273732569204197 (Allowable error: 0.1%, Actual error: 2.5%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.24173102578453243 but the right hand side evaluated to 0.17660075377550288 (Allowable error: 0.1%, Actual error: 1.4%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.430223423657364 but the right hand side evaluated to 4.666980921964073 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.495475412264772 but the right hand side evaluated to 4.696716927188014 (Allowable error: 0.1%, Actual error: 37%)


Solves with these variables bounded:
   value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission

Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... &gt;= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2481462.81141 force_pound * meter but the right hand side evaluated to 2426091.29204 force_pound * meter (Allowable error: 0.1%, Actual error: 2.3%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... &gt;= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.3977688 force_pound but the right hand side evaluated to 32399.9999953 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... &gt;= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116651 meter but the right hand side evaluated to 1.83120538694 meter (Allowable error: 0.1%, Actual error: 17%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1203375.3999 joule / kilogram but the right hand side evaluated to 1.66378771145 megajoule / kilogram (Allowable error: 0.1%, Actual error: 17%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... &gt;= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4693765751 meter but the right hand side evaluated to 16.6431965782 meter (Allowable error: 0.1%, Actual error: 11%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 11.047303631439933 but the right hand side evaluated to 4.801800726246141 (Allowable error: 0.1%, Actual error: 57%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 9.670705608939397 but the right hand side evaluated to 4.801800695865673 (Allowable error: 0.1%, Actual error: 50%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.221369907176056 but the right hand side evaluated to 4.801800735381865 (Allowable error: 0.1%, Actual error: 42%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.6280031295 meter but the right hand side evaluated to 18.3449813647 meter (Allowable error: 0.1%, Actual error: 1.5%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.6280031295 meter but the right hand side evaluated to 18.4743883475 meter (Allowable error: 0.1%, Actual error: 0.82%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3268323026901063 but the right hand side evaluated to 0.19660249204375774 (Allowable error: 0.1%, Actual error: 2.8%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.25274921954141494 but the right hand side evaluated to 0.17938776044576993 (Allowable error: 0.1%, Actual error: 1.5%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.455613773807696 but the right hand side evaluated to 4.729213696681945 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.548870526111195 but the right hand side evaluated to 4.762573952725038 (Allowable error: 0.1%, Actual error: 37%)


Solves with these variables bounded:
   value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission

Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... &gt;= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2455568.28987 force_pound * meter but the right hand side evaluated to 2407712.11105 force_pound * meter (Allowable error: 0.1%, Actual error: 2%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... &gt;= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4677599 force_pound but the right hand side evaluated to 32399.9999996 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... &gt;= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116811 meter but the right hand side evaluated to 1.99552044649 meter (Allowable error: 0.1%, Actual error: 9.9%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1227633.98642 joule / kilogram but the right hand side evaluated to 1.72359781608 megajoule / kilogram (Allowable error: 0.1%, Actual error: 18%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 677538.860978 joule / kilogram but the right hand side evaluated to 0.67918187724 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.11%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... &gt;= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4156358879 meter but the right hand side evaluated to 16.4239739827 meter (Allowable error: 0.1%, Actual error: 12%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.974970489407543 but the right hand side evaluated to 4.762555682431843 (Allowable error: 0.1%, Actual error: 57%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 9.752897401039991 but the right hand side evaluated to 4.76255567815332 (Allowable error: 0.1%, Actual error: 51%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.158719172125435 but the right hand side evaluated to 4.762555683558495 (Allowable error: 0.1%, Actual error: 42%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4488734457 meter but the right hand side evaluated to 18.204663784 meter (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4488734457 meter but the right hand side evaluated to 18.3176205464 meter (Allowable error: 0.1%, Actual error: 0.71%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.30594675075750644 but the right hand side evaluated to 0.19198937433671495 (Allowable error: 0.1%, Actual error: 2.4%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.23933863285315926 but the right hand side evaluated to 0.17598609850329125 (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.504819810313443 but the right hand side evaluated to 4.6997843766612775 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.527659915142774 but the right hand side evaluated to 4.728945718712703 (Allowable error: 0.1%, Actual error: 37%)


Solves with these variables bounded:
   value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission

Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... &gt;= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2436785.14858 force_pound * meter but the right hand side evaluated to 2390898.65856 force_pound * meter (Allowable error: 0.1%, Actual error: 1.9%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... &gt;= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4890489 force_pound but the right hand side evaluated to 32399.9999987 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... &gt;= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116794 meter but the right hand side evaluated to 2.03201248014 meter (Allowable error: 0.1%, Actual error: 8.3%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1233975.55083 joule / kilogram but the right hand side evaluated to 1.62326527734 megajoule / kilogram (Allowable error: 0.1%, Actual error: 15%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... &gt;= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4095776716 meter but the right hand side evaluated to 16.3813501337 meter (Allowable error: 0.1%, Actual error: 12%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.931050687394404 but the right hand side evaluated to 4.787717407907646 (Allowable error: 0.1%, Actual error: 56%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 9.873363204878085 but the right hand side evaluated to 4.787717400062887 (Allowable error: 0.1%, Actual error: 52%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.154646845064601 but the right hand side evaluated to 4.787717410081996 (Allowable error: 0.1%, Actual error: 41%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4102707197 meter but the right hand side evaluated to 18.1746816433 meter (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4102707197 meter but the right hand side evaluated to 18.2839307157 meter (Allowable error: 0.1%, Actual error: 0.69%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.30209841964199935 but the right hand side evaluated to 0.19112016137014207 (Allowable error: 0.1%, Actual error: 2.3%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.2368540362284266 but the right hand side evaluated to 0.17534417530554194 (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.536485120144714 but the right hand side evaluated to 4.72672170530791 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.5513986884521875 but the right hand side evaluated to 4.755134305410748 (Allowable error: 0.1%, Actual error: 37%)


Solves with these variables bounded:
   value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission

Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... &gt;= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2418323.70656 force_pound * meter but the right hand side evaluated to 2374882.64553 force_pound * meter (Allowable error: 0.1%, Actual error: 1.8%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... &gt;= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.5227007 force_pound but the right hand side evaluated to 32399.999997 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... &gt;= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116755 meter but the right hand side evaluated to 2.08235073222 meter (Allowable error: 0.1%, Actual error: 6%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1244505.01726 joule / kilogram but the right hand side evaluated to 1.55924161703 megajoule / kilogram (Allowable error: 0.1%, Actual error: 12%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 664748.646964 joule / kilogram but the right hand side evaluated to 0.667399666439 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.18%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... &gt;= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4000487549 meter but the right hand side evaluated to 16.3223837535 meter (Allowable error: 0.1%, Actual error: 13%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.904034918476636 but the right hand side evaluated to 4.7895015223081945 (Allowable error: 0.1%, Actual error: 56%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 10.025966540210804 but the right hand side evaluated to 4.789501505152584 (Allowable error: 0.1%, Actual error: 52%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.14555593747884 but the right hand side evaluated to 4.789501527007668 (Allowable error: 0.1%, Actual error: 41%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.3618041636 meter but the right hand side evaluated to 18.1374340984 meter (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.3618041636 meter but the right hand side evaluated to 18.2416923767 meter (Allowable error: 0.1%, Actual error: 0.65%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.2959618215655109 but the right hand side evaluated to 0.18972196428612648 (Allowable error: 0.1%, Actual error: 2.2%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.232977239782163 but the right hand side evaluated to 0.17433509371429662 (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.565342863472917 but the right hand side evaluated to 4.7313160166037855 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.583811962471225 but the right hand side evaluated to 4.75851274462609 (Allowable error: 0.1%, Actual error: 37%)


Solves with these variables bounded:
   value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission

Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... &gt;= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2405735.09617 force_pound * meter but the right hand side evaluated to 2358168.31156 force_pound * meter (Allowable error: 0.1%, Actual error: 2%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... &gt;= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4381517 force_pound but the right hand side evaluated to 32399.9999991 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... &gt;= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116809 meter but the right hand side evaluated to 1.97491000622 meter (Allowable error: 0.1%, Actual error: 11%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1245747.32228 joule / kilogram but the right hand side evaluated to 1.35773023721 megajoule / kilogram (Allowable error: 0.1%, Actual error: 4.7%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... &gt;= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4441337653 meter but the right hand side evaluated to 16.4749777907 meter (Allowable error: 0.1%, Actual error: 12%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.933107627325658 but the right hand side evaluated to 4.831717386535661 (Allowable error: 0.1%, Actual error: 56%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 10.192138959197969 but the right hand side evaluated to 4.831717368232709 (Allowable error: 0.1%, Actual error: 53%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.195656247771407 but the right hand side evaluated to 4.831717390218115 (Allowable error: 0.1%, Actual error: 41%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4861302525 meter but the right hand side evaluated to 18.2368501098 meter (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4861302525 meter but the right hand side evaluated to 18.3518650106 meter (Allowable error: 0.1%, Actual error: 0.73%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3102024631761644 but the right hand side evaluated to 0.19294188893841294 (Allowable error: 0.1%, Actual error: 2.5%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.2419212810602822 but the right hand side evaluated to 0.17664947460760705 (Allowable error: 0.1%, Actual error: 1.4%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.542128652286824 but the right hand side evaluated to 4.76697799126954 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.59702352627845 but the right hand side evaluated to 4.797042037273719 (Allowable error: 0.1%, Actual error: 37%)


Solves with these variables bounded:
   value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission

Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... &gt;= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2391779.91091 force_pound * meter but the right hand side evaluated to 2346059.36115 force_pound * meter (Allowable error: 0.1%, Actual error: 1.9%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... &gt;= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.380752 force_pound but the right hand side evaluated to 32399.999999 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... &gt;= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116807 meter but the right hand side evaluated to 2.01208200498 meter (Allowable error: 0.1%, Actual error: 9.2%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1263254.57361 joule / kilogram but the right hand side evaluated to 1.32933786803 megajoule / kilogram (Allowable error: 0.1%, Actual error: 2.8%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 643003.170869 joule / kilogram but the right hand side evaluated to 0.644587782568 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.11%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... &gt;= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4391885939 meter but the right hand side evaluated to 16.4333016913 meter (Allowable error: 0.1%, Actual error: 12%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.92705813493721 but the right hand side evaluated to 4.827096736211918 (Allowable error: 0.1%, Actual error: 56%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 10.332849377438421 but the right hand side evaluated to 4.827096714740888 (Allowable error: 0.1%, Actual error: 53%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.188196577296955 but the right hand side evaluated to 4.827096741334141 (Allowable error: 0.1%, Actual error: 41%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4531699214 meter but the right hand side evaluated to 18.212378902 meter (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4531699214 meter but the right hand side evaluated to 18.3237361088 meter (Allowable error: 0.1%, Actual error: 0.7%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.30544730461879066 but the right hand side evaluated to 0.19187565477574478 (Allowable error: 0.1%, Actual error: 2.4%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.23886094945446779 but the right hand side evaluated to 0.17586358419152223 (Allowable error: 0.1%, Actual error: 1.3%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.5542886212927876 but the right hand side evaluated to 4.764561623928035 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.617832768153137 but the right hand side evaluated to 4.793693912308904 (Allowable error: 0.1%, Actual error: 37%)


Solves with these variables bounded:
   value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission

Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... &gt;= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2376282.70615 force_pound * meter but the right hand side evaluated to 2334599.75536 force_pound * meter (Allowable error: 0.1%, Actual error: 1.8%)

Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... &gt;= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4774522 force_pound but the right hand side evaluated to 32399.9999988 force_pound (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... &gt;= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116802 meter but the right hand side evaluated to 2.09817184356 meter (Allowable error: 0.1%, Actual error: 5.3%)

Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... &lt;= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1283640.91157 joule / kilogram but the right hand side evaluated to 1.28936004152 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.24%)

Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... &gt;= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4146013604 meter but the right hand side evaluated to 16.3183418346 meter (Allowable error: 0.1%, Actual error: 13%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.937464499355212 but the right hand side evaluated to 4.8243790893834015 (Allowable error: 0.1%, Actual error: 56%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 10.571347254923474 but the right hand side evaluated to 4.8243790790080725 (Allowable error: 0.1%, Actual error: 54%)

Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.193851603784035 but the right hand side evaluated to 4.824379092042728 (Allowable error: 0.1%, Actual error: 41%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.3565588973 meter but the right hand side evaluated to 18.1377550189 meter (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... &gt;= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.3565588973 meter but the right hand side evaluated to 18.2401789494 meter (Allowable error: 0.1%, Actual error: 0.63%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.29417340619954313 but the right hand side evaluated to 0.18931100276733917 (Allowable error: 0.1%, Actual error: 2.2%)

Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... &gt;= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.23165673547385524 but the right hand side evaluated to 0.1739892876586922 (Allowable error: 0.1%, Actual error: 1.2%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.620071288870777 but the right hand side evaluated to 4.76702011382697 (Allowable error: 0.1%, Actual error: 37%)

Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... &gt;= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.689393257365433 but the right hand side evaluated to 4.793939483758628 (Allowable error: 0.1%, Actual error: 38%)


Solves with these variables bounded:
   value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct
   value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission

Sweeping took 1.45e+03 seconds.

Running tests...
----------------------------------------------------------------------
.
----------------------------------------------------------------------
Ran 1 test in 1456.996s

OK

Generating XML reports...
Cloning into 'solar'...
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1)
Requirement already satisfied: pytz&gt;=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3)
Requirement already satisfied: numpy&gt;=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.2)
Requirement already satisfied: six&gt;=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil-&gt;pandas) (1.11.0)
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
Collecting git+<a href='https://github.com/convexengineering/gpfit.git'>https://github.com/convexengineering/gpfit.git</a>
  Cloning <a href='https://github.com/convexengineering/gpfit.git'>https://github.com/convexengineering/gpfit.git</a> to c:\users\jenkins\appdata\local\temp\pip-req-build-_pqodl
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+<a href='https://github.com/convexengineering/gpfit.git'>https://github.com/convexengineering/gpfit.git</a> in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint&gt;=0.7 in d:\anaconda2\lib\site-packages (from gpkit-&gt;gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit-&gt;gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
  Running setup.py bdist_wheel for gpfit: started
  Running setup.py bdist_wheel for gpfit: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-tda79e\wheels\d5\94\ac\b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12
Successfully built gpfit
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
Collecting git+<a href='https://github.com/convexengineering/gassolar.git'>https://github.com/convexengineering/gassolar.git</a>
  Cloning <a href='https://github.com/convexengineering/gassolar.git'>https://github.com/convexengineering/gassolar.git</a> to c:\users\jenkins\appdata\local\temp\pip-req-build-thrckh
Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+<a href='https://github.com/convexengineering/gassolar.git'>https://github.com/convexengineering/gassolar.git</a> in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1)
Requirement already satisfied: pint&gt;=0.7 in d:\anaconda2\lib\site-packages (from gpkit-&gt;gassolar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit-&gt;gassolar==0.0.0.0) (1.3.2)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas-&gt;gassolar==0.0.0.0) (2.6.1)
Requirement already satisfied: pytz&gt;=2011k in d:\anaconda2\lib\site-packages (from pandas-&gt;gassolar==0.0.0.0) (2017.3)
Requirement already satisfied: six&gt;=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil-&gt;pandas-&gt;gassolar==0.0.0.0) (1.11.0)
Building wheels for collected packages: gassolar
  Running setup.py bdist_wheel for gassolar: started
  Running setup.py bdist_wheel for gassolar: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-efdwwv\wheels\fe\11\0a\2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e
Successfully built gassolar
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
Processing d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\solar
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit (from solar==0.0.0.0) (0.7.0.0)
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (0.22.0)
Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from solar==0.0.0.0) (0.1)
Requirement already satisfied: gpkitmodels in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek (from solar==0.0.0.0) (0.0.0.0)
Requirement already satisfied: pint&gt;=0.7 in d:\anaconda2\lib\site-packages (from gpkit-&gt;solar==0.0.0.0) (0.8.1)
Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit-&gt;solar==0.0.0.0) (1.3.2)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas-&gt;solar==0.0.0.0) (2.6.1)
Requirement already satisfied: pytz&gt;=2011k in d:\anaconda2\lib\site-packages (from pandas-&gt;solar==0.0.0.0) (2017.3)
Requirement already satisfied: six&gt;=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil-&gt;pandas-&gt;solar==0.0.0.0) (1.11.0)
Building wheels for collected packages: solar
  Running setup.py bdist_wheel for solar: started
  Running setup.py bdist_wheel for solar: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-xzh4qr\wheels\09\7a\4a\77e70a4d3b01c71b043502f2bf60681f14786c725c35efc56c
Successfully built solar
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
Installing collected packages: solar
Successfully installed solar-0.0.0.0
adding test for 'solar/solar.py'
adding test for 'solar/sens_chart.py'
adding test for 'solar/season.py'
Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,).
Using solver 'mosek'
Solving for 9147 variables.
Solving took 3.56 seconds.
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1624 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0315 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0339 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1624 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0315 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0339 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(3,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(4,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(2,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(0,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(1,).
Using solver 'mosek'
Solving for 9147 variables.
Solving took 15.6 seconds.
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(0,).
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(3,).
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(4,).
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(2,).
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(1,).
Using solver 'mosek'
Solving for 9147 variables.
Solving took 11.1 seconds.
Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 625493.8994 but bound is 600000.0000
Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460
Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0324 but bound is 0.0500
Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0352 but bound is 0.0500
Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460
Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0324 but bound is 0.0500
Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0352 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(3,).
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(1,).
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(2,).
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(4,).
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(0,).
Using solver 'mosek'
Solving for 4707 variables.
Solving took 4.55 seconds.
Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 642574.9335 but bound is 600000.0000
Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500
Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,).
Using solver 'mosek'
Solving for 9147 variables.
Solving took 11.3 seconds.
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1624 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0315 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0339 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1624 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0315 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0339 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(3,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(4,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(2,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(0,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(1,).
Using solver 'mosek'
Solving for 9147 variables.
Solving took 33.7 seconds.
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1666 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0320 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0346 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(0,).
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(3,).
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(4,).
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(2,).
Couldn't auto-differentiate linked variable rho_Mission.2/Climb.2_(1,).
Using solver 'mosek'
Solving for 9147 variables.
Solving took 9.28 seconds.
Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 625493.9680 but bound is 600000.0000
Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460
Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0324 but bound is 0.0500
Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0352 but bound is 0.0500
Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460
Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0324 but bound is 0.0500
Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0352 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(3,).
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(1,).
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(2,).
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(4,).
Couldn't auto-differentiate linked variable rho_Mission.3/Climb.3_(0,).
Using solver 'mosek'
Solving for 4707 variables.
Solving took 1.92 seconds.
Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 642574.9338 but bound is 600000.0000
Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500
Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500
Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,).
Using solver 'mosek'
Solving for 489 variables.
Solving took 18.7 seconds.
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 642574.3921 but bound is 600000.0000
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,).
Using solver 'mosek'
Solving for 489 variables.
Solving took 1.87 seconds.
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 642574.3920 but bound is 600000.0000
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,).
Using solver 'mosek'
Solving for 4707 variables.
Solving took 24.3 seconds.
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 642574.9384 but bound is 600000.0000
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(3,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(4,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(2,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(0,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(1,).
Beginning signomial solve.
Solving took 4 GP solves and 38.1 seconds.
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), Re_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is above upper bound. Solution is 641279.3556 but bound is 600000.0000
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0251 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0368 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0251 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0368 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission/Climb_(3,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(1,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(2,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(0,).
Couldn't auto-differentiate linked variable rho_Mission/Climb_(4,).
Using solver 'mosek_cli'
Solving for 4707 variables.
Solving took 62.2 seconds.
Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 642575.7579 but bound is 600000.0000
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1741 but bound is 0.1460
Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0330 but bound is 0.0500
Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0357 but bound is 0.0500
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(3,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(4,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(2,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(0,).
Couldn't auto-differentiate linked variable rho_Mission.1/Climb.1_(1,).
Beginning signomial solve.
Solving took 4 GP solves and 221 seconds.
Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), Re_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is above upper bound. Solution is 641279.0650 but bound is 600000.0000
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0251 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0368 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.1713 but bound is 0.1460
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0251 but bound is 0.0500
Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0368 but bound is 0.0500

Running tests...
----------------------------------------------------------------------
D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp
  tau = np.exp(-0.175/costhsun)
D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide
  tau = np.exp(-0.175/costhsun)
......
----------------------------------------------------------------------
Ran 6 tests in 756.964s

OK

Generating XML reports...
Cloning into 'gplibrary'...
Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.22.0)
Requirement already satisfied: python-dateutil in d:\anaconda2\lib\site-packages (from pandas) (2.6.1)
Requirement already satisfied: pytz&gt;=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3)
Requirement already satisfied: numpy&gt;=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.2)
Requirement already satisfied: six&gt;=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil-&gt;pandas) (1.11.0)
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
Collecting git+<a href='https://github.com/hoburg/gpfit.git'>https://github.com/hoburg/gpfit.git</a>
  Cloning <a href='https://github.com/hoburg/gpfit.git'>https://github.com/hoburg/gpfit.git</a> to c:\users\jenkins\appdata\local\temp\pip-req-build-kzaydd
Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+<a href='https://github.com/hoburg/gpfit.git'>https://github.com/hoburg/gpfit.git</a> in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages
Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.0.1)
Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gpkit (from gpfit==0.1) (0.7.0.0)
Requirement already satisfied: pint&gt;=0.7 in d:\anaconda2\lib\site-packages (from gpkit-&gt;gpfit==0.1) (0.8.1)
Requirement already satisfied: ad in d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\venv2_gpkit\lib\site-packages (from gpkit-&gt;gpfit==0.1) (1.3.2)
Building wheels for collected packages: gpfit
  Running setup.py bdist_wheel for gpfit: started
  Running setup.py bdist_wheel for gpfit: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-svvvui\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f
Successfully built gpfit
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
Processing d:\jenkins\workspace\gplibrary_pr_models\buildnode\windows7x64\optimizer\mosek\gplibrary
Requirement already satisfied: numpy&gt;=1.12 in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.2)
Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.0.1)
Requirement already satisfied: pint in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (0.8.1)
Building wheels for collected packages: gpkitmodels
  Running setup.py bdist_wheel for gpkitmodels: started
  Running setup.py bdist_wheel for gpkitmodels: finished with status 'done'
  Stored in directory: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-hnt5nd\wheels\92\ce\06\ec49b09e82f01f946f52378df5a542ddac6d03b78d4466cd8e
Successfully built gpkitmodels
grin 1.2.1 requires argparse&gt;=1.1, which is not installed.
Installing collected packages: gpkitmodels
  Found existing installation: gpkitmodels 0.0.0.0
    Uninstalling gpkitmodels-0.0.0.0:
      Successfully uninstalled gpkitmodels-0.0.0.0
Successfully installed gpkitmodels-0.0.0.0
adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py'
adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py'
adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py'
adding test for 'gpkitmodels/GP/aircraft/prop/prop_test.py'
Using solver 'mosek'
Solving for 11 variables.
Solving took 14.8 seconds.
Using solver 'mosek_cli'
Solving for 11 variables.
Solving took 1.74 seconds.
Using solver 'mosek'
Solving for 5 variables.
Solving took 0.027 seconds.
Using solver 'mosek_cli'
Solving for 5 variables.
Solving took 1 seconds.
Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3481 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9721 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2223878.3856 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2223877.9562 but bound is 1000000.0000
Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000
Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000
Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1884891.4063 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656770.2552 but bound is 700000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000

Running tests...
----------------------------------------------------------------------
........
----------------------------------------------------------------------
Ran 8 tests in 75.156s

OK

Generating XML reports...
Cloning into 'eVTOL'...
adding test for 'aircraft_models.py'

Running tests...
----------------------------------------------------------------------
..
----------------------------------------------------------------------
Ran 2 tests in 22.955s

OK

Generating XML reports...
USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY
calling ['pip', 'install', '--no-cache-dir', '--no-deps', '-e', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', '<a href='https://github.com/convexengineering/shopping.git'>https://github.com/convexengineering/shopping.git</a>']
  attempt 1

SETTINGS
defaultdict(&lt;type 'str'&gt;, {})

calling ['git', 'clone', '--depth', '1', '-b', 'master', '<a href='https://github.com/convexengineering/gassolar.git'>https://github.com/convexengineering/gassolar.git</a>']
  attempt 1

SETTINGS
defaultdict(&lt;type 'str'&gt;, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+<a href='https://github.com/hoburg/gpfit.git'>https://github.com/hoburg/gpfit.git</a>', 'gpkit-models branch': 'master'})

calling ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+<a href='https://github.com/hoburg/gpfit.git'>https://github.com/hoburg/gpfit.git</a>']
  attempt 1
calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', '<a href='https://github.com/convexengineering/jho.git'>https://github.com/convexengineering/jho.git</a>']
  attempt 1

SETTINGS
defaultdict(&lt;type 'str'&gt;, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+<a href='https://github.com/hoburg/gpfit.git'>https://github.com/hoburg/gpfit.git</a>', 'gpkit-models branch': 'master'})

calling ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+<a href='https://github.com/hoburg/gpfit.git'>https://github.com/hoburg/gpfit.git</a>']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', '<a href='https://github.com/convexengineering/turbofan.git'>https://github.com/convexengineering/turbofan.git</a>']
  attempt 1

SETTINGS
defaultdict(&lt;type 'str'&gt;, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'})

calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', '<a href='https://github.com/convexengineering/SPaircraft.git'>https://github.com/convexengineering/SPaircraft.git</a>']
  attempt 1

SETTINGS
defaultdict(&lt;type 'str'&gt;, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+<a href='https://github.com/hoburg/turbofan.git'>https://github.com/hoburg/turbofan.git</a>', 'gpkit-models branch': 'master'})

calling ['pip', 'install', 'git+<a href='https://github.com/hoburg/turbofan.git'>https://github.com/hoburg/turbofan.git</a>']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', '<a href='https://github.com/convexengineering/solar.git'>https://github.com/convexengineering/solar.git</a>']
  attempt 1

SETTINGS
defaultdict(&lt;type 'str'&gt;, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+<a href='https://github.com/convexengineering/gpfit.git'>https://github.com/convexengineering/gpfit.git</a>, git+<a href='https://github.com/convexengineering/gassolar.git'>https://github.com/convexengineering/gassolar.git</a>', 'gpkit-models branch': 'master'})

calling ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+<a href='https://github.com/convexengineering/gpfit.git'>https://github.com/convexengineering/gpfit.git</a>']
  attempt 1
calling ['pip', 'install', 'git+<a href='https://github.com/convexengineering/gassolar.git'>https://github.com/convexengineering/gassolar.git</a>']
  attempt 1
calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', '<a href='https://github.com/convexengineering/gplibrary.git'>https://github.com/convexengineering/gplibrary.git</a>']
  attempt 1

SETTINGS
defaultdict(&lt;type 'str'&gt;, {'pip install': 'pandas, git+<a href='https://github.com/hoburg/gpfit.git&#39;}'>https://github.com/hoburg/gpfit.git'}</a>)

calling ['pip', 'install', 'pandas']
  attempt 1
calling ['pip', 'install', 'git+<a href='https://github.com/hoburg/gpfit.git'>https://github.com/hoburg/gpfit.git</a>']
  attempt 1
calling ['pip', 'install', '.']
  attempt 1
calling ['git', 'clone', '--depth', '1', '-b', 'master', '<a href='https://github.com/convexengineering/eVTOL.git'>https://github.com/convexengineering/eVTOL.git</a>']
  attempt 1

SETTINGS
defaultdict(&lt;type 'str'&gt;, {})


(venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek&gt;exit 0 
[xUnit] [INFO] - Starting to record.
[xUnit] [INFO] - Processing JUnit
[xUnit] [INFO] - [JUnit] - 8 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to 'D:\jenkins\workspace\gplibrary_PR_Models\buildnode\windows7x64\optimizer\mosek' for the testing framework 'JUnit'.
[xUnit] [INFO] - Check 'Failed Tests' threshold.
[xUnit] [INFO] - Check 'Skipped Tests' threshold.
[xUnit] [INFO] - Setting the build status to SUCCESS
[xUnit] [INFO] - Stopping recording.
[WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done
Finished: SUCCESS